FR2643947B1 - Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable - Google Patents

Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable

Info

Publication number
FR2643947B1
FR2643947B1 FR8902640A FR8902640A FR2643947B1 FR 2643947 B1 FR2643947 B1 FR 2643947B1 FR 8902640 A FR8902640 A FR 8902640A FR 8902640 A FR8902640 A FR 8902640A FR 2643947 B1 FR2643947 B1 FR 2643947B1
Authority
FR
France
Prior art keywords
turboreactor
push
variable section
ejection assembly
axisymmetrical
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
FR8902640A
Other languages
English (en)
Other versions
FR2643947A1 (fr
Inventor
Alain Marie Joseph Lardellier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR8902640A priority Critical patent/FR2643947B1/fr
Priority to EP90400502A priority patent/EP0385834B1/fr
Priority to DE9090400502T priority patent/DE69001500T2/de
Priority to US07/486,851 priority patent/US4993638A/en
Publication of FR2643947A1 publication Critical patent/FR2643947A1/fr
Application granted granted Critical
Publication of FR2643947B1 publication Critical patent/FR2643947B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8902640A 1989-03-01 1989-03-01 Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable Expired - Lifetime FR2643947B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8902640A FR2643947B1 (fr) 1989-03-01 1989-03-01 Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable
EP90400502A EP0385834B1 (fr) 1989-03-01 1990-02-23 Ensemble d'éjection de Turboréacteur à tuyère axisymétrique à section variable et à poussée orientable
DE9090400502T DE69001500T2 (de) 1989-03-01 1990-02-23 Verstell- und neigbare schubdueseneinheit fuer ein strahltriebwerk.
US07/486,851 US4993638A (en) 1989-03-01 1990-03-01 Thrust vectoring nozzle assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8902640A FR2643947B1 (fr) 1989-03-01 1989-03-01 Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable

Publications (2)

Publication Number Publication Date
FR2643947A1 FR2643947A1 (fr) 1990-09-07
FR2643947B1 true FR2643947B1 (fr) 1991-05-17

Family

ID=9379242

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8902640A Expired - Lifetime FR2643947B1 (fr) 1989-03-01 1989-03-01 Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable

Country Status (4)

Country Link
US (1) US4993638A (fr)
EP (1) EP0385834B1 (fr)
DE (1) DE69001500T2 (fr)
FR (1) FR2643947B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5294055A (en) * 1992-09-08 1994-03-15 Mcdonnell Douglas Corporation Rotatable arms for thrust vectoring and changing the area of a nozzle throat
RU2037066C1 (ru) * 1993-10-01 1995-06-09 Владимир Павлович Знаменский Способ получения тяги и устройство для его осуществления
GB2356897B (en) * 1999-12-01 2003-05-14 Secr Defence Improved nozzle
US20090090817A1 (en) * 2007-10-09 2009-04-09 Monka Gary H Aircraft configuration, gas turbine engine, controller and trim system for neutralizing pitching moments with power changes
DE102008022271A1 (de) 2008-05-06 2009-11-26 Opara, Günther Düse für einen Strömungsantrieb
TWI715227B (zh) * 2019-09-30 2021-01-01 林瑤章 飛行載具及其推進裝置
US10837402B2 (en) 2020-01-09 2020-11-17 Guanhao Wu Thrust vector nozzle
CN113799990A (zh) * 2020-06-17 2021-12-17 林瑶章 具双层导流组件的推进装置及具有其的飞行载具
CN114718757A (zh) * 2022-03-23 2022-07-08 西北工业大学 一种微型涡喷发动机尾喷管设计方案

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR68790E (fr) * 1955-12-29 1958-06-10 Aerotecnica Aérodyne à voilure tournante
FR1153561A (fr) * 1956-06-01 1958-03-12 Nouveau mode de propulsion à réaction pour les engins marins et nouveau déviateur de jet
FR1303806A (fr) * 1961-10-16 1962-09-14 D Aviat Latecoere Soc Ind Dispositif déviateur de jet pour l'orientation et la stabilisation d'un engin pendant la phase d'atterrissage
US3130544A (en) * 1961-10-23 1964-04-28 Salvatore J Penza Variable thrust and direction nozzle
GB1139958A (en) * 1966-11-30 1969-01-15 Rolls Royce Jet nozzle assembly for a gas turbine engine
DE1993361U (de) * 1968-04-25 1968-09-05 Ver Flugtechnische Werke G M B Ablenkvorrichtung fuer insbesondere heisse abgasstrahlen an flugzeugtriebwerken.
US3912202A (en) * 1974-06-17 1975-10-14 Lockheed Aircraft Corp Side force control for airplanes
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
FR2501786A1 (fr) * 1981-03-13 1982-09-17 Snecma Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction
JPS60237147A (ja) * 1984-05-09 1985-11-26 Toru Fujii ゼット航空機の無尾翼方式制御
FR2608680B1 (fr) * 1986-12-17 1989-03-17 Snecma Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion
DE3643823A1 (de) * 1986-12-20 1988-06-30 Messerschmitt Boelkow Blohm Schubvektorsteuerung fuer luftfahrzeuge

Also Published As

Publication number Publication date
EP0385834A1 (fr) 1990-09-05
DE69001500T2 (de) 1993-09-23
EP0385834B1 (fr) 1993-05-05
FR2643947A1 (fr) 1990-09-07
US4993638A (en) 1991-02-19
DE69001500D1 (de) 1993-06-09

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